PID: Billy-Integral-Differential When the multi-rotor aircraft has any angle change on the PITCH/ROLL/YAW axis, the gyroscope will output the deviation angle value relative to the initial position. The flight control uses the \"PID\" program algorithm to drive the motor based on the recorded original position to return the multi-rotor aircraft to the initial position. This is a combination of data sampling over time and predicting future positions based on the measured angle deviation. The information it provides is enough for the flight control to drive the motor to return the multi-rotor aircraft to a balanced state. The P value is the most important part of the PID, which directly determines the flight effect of the aircraft.
You Might Like
Recommended ContentMore
Open source project More
Popular Components
Searched by Users
Just Take a LookMore
Trending Downloads
Trending ArticlesMore